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035   $a(EXLCZ)995470000002504901
100   $a20190610d1956      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis and comparison with theory of flow-field measurements near a lifting rotor in the Langley full-scale tunnel /$fby Harry H. Heyson
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1956.
215   $a1 online resource (162 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3691
300   $a"April 1956.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 15-16).
606   $aAir flow
606   $aRotors (Helicopters)
606   $aWakes (Aerodynamics)$xMeasurement
606   $aWind tunnel testing
606   $aAir flow$2fast
606   $aRotors (Helicopters)$2fast
606   $aWakes (Aerodynamics)$xMeasurement$2fast
606   $aWind tunnel testing$2fast
615  0$aAir flow.
615  0$aRotors (Helicopters)
615  0$aWakes (Aerodynamics)$xMeasurement.
615  0$aWind tunnel testing.
615  7$aAir flow.
615  7$aRotors (Helicopters)
615  7$aWakes (Aerodynamics)$xMeasurement.
615  7$aWind tunnel testing.
700   $aHeyson$b Harry H.$0299122
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713879003321
996   $aAnalysis and comparison with theory of flow-field measurements near a lifting rotor in the Langley full-scale tunnel$93444230
997   $aUNINA